NORSAT 4, 62702
Orbit data source: Space-Track
NORSAT 4, 62702 is a payload satellite owned by NSC (NO) in SSO that was launched on Tue, 14 Jan 2025 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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62702 intel report (Beta)
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Identifier
Orbit
Country
NO / NORRelated business
Manufacturer
UTIAS-SFL
Mission
Operational Civil Com/Tech
Bus & Motor
DEFIANT, Unknown motor
Mass
35 kg wet, 35 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.3 m
Radar Cross Section
0.165 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 17 hours ago
TLE from 17 hours ago
0 NORSAT 4
1 62702U 25009CX 26255.64716964 .00001370 00000-0 12945-3 0 9991
2 62702 97.6992 332.8109 0003211 98.3244 261.8341 14.95305290 90433Epoch: 2026-09-12T15:31Z
TLE epoch observation values (Epoch: 2026-09-12T15:31:55.456Z)
Latitude
-0.00005°
Longitude
108.17667°
Altitude
584.792 km
Speed
7.568 km/s
True Right ascension
22h 11m 14s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
01:09:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
580.671 km
Perigee altitude
576.203 km
Semi-major axis
6,956.574 km
Eccentricity
0.00032
Inclination
97.6992°
RAAN
332.8109°
Arg. of periapsis
98.3244°
True anomaly
261.79768°
Mean anomaly
261.8341°
Eccentric anomaly
261.81589°
Mean motion
3.74068 °/min
Orbital period
96.24 mins
BSTAR
0.00012945
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Other satellites on launch #9 in the year 2025 (2025-01-14 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.NORSAT 4 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-09-13 17:48:03.024Z | 26.232° NE | 2026-09-13 17:51:03.024Z | 88.13° E | 50.883° | 2026-09-13 17:55:03.024Z | 176.005° S |
| 6 mins | 2026-09-14 04:37:03.024Z | 122.431° SE | 2026-09-14 04:39:03.024Z | 84.625° E | 29.47° | 2026-09-14 04:43:03.024Z | 9.897° NNE |
| 4 mins | 2026-09-14 06:13:03.024Z | 232.096° WSW | 2026-09-14 06:15:03.024Z | 268.797° W | 19.891° | 2026-09-14 06:17:03.024Z | 303.585° NW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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